Gulfstream Flashlight Installation Instructions
Model: AVE-MOD-016-INS, Issue 02
Applicable to Gulfstream Aircraft:
- Gulfstream GII, GIII, GIV & GV
- Gulfstream GVI
- Gulfstream G150
- Gulfstream G200 / Galaxy
- Gulfstream G280
Part 0: Manual Administration
0.1 Document Approval
This document has been established in accordance with an alternative procedure to DOA approved under EASA AP429. This installation instruction is applicable for all Gulfstream types.
Compiled by: Peter Nezval, Engineer, Aveo Engineering Group, s.r.o. (Date: 17. Jul. 2017)
Approved by: Georg Hartl, Head of DO, Aveo Engineering Group, s.r.o. (Date: 17. Jul. 2017)
0.2 Amendment Record Procedure
The master copy of this document is kept electronically as a read-only document under the control of Aveo Engineering Group, s.r.o. All amendments initiate a raise of issue, with sequential alphabetic issue identifiers from 01 to 99. The initial issue is "01". All issues are approved by the Head of DO.
| Issue No. | Details | Date | Effected Pages |
|---|---|---|---|
| 01 | Initial Issue | 14.Jun.2017 | ALL |
| 02 | Change Title and add list of aircraft types (not marked) | 17.Jul.2014 | 1 |
0.3 Effected Pages Procedure
All pages affected by any issue raise are listed in the 'Effected Pages Column' of Table 01. The reasons and descriptions for changes are provided in the 'Details Column' of Table 01. Changes from the previous issue are highlighted by yellow highlighting for new content and yellow highlighting with crossing out for deleted content.
Part 1: Installation Instruction
1.1 General
This installation is to be performed in accordance with common practice described in the general practice section of the respective Gulfstream Aircraft Maintenance Manual. The installer must follow the latest revision of the following documents:
- Gulfstream AMM
- AVE-FLA070-IM
No specific drawings are applicable for this change. The following appliances carry an ETSO authorization: None. The change is to be performed using document AVE-MOD-016-MCS in its latest issue. Aircraft manuals remain valid; for maintenance of the new lights, follow the referenced Aveo Installation Manuals.
1.2 Continued Airworthiness
Aircraft manuals remain fully valid. Inspection intervals and procedures of the aircraft override general statements in component manuals listed under §1.1. For inspection of the new lights, follow the procedure in the referenced Aveo Installation Manuals.
1.3 Description
This modification involves replacing the existing flashlights and their chargers. The installation includes two units in the cockpit and one unit in the baggage compartment. The new lights are direct replacements and do not require any changes to the aircraft's electrical system (A/C side).
1.4 Flashlight Installation
The installation involves mounting the flashlight and its cradle/charger. The process is detailed across several diagrams and a parts list.
Diagrammatic Representation of Installation:
Aircraft Overview
A diagram shows a side profile of a Gulfstream aircraft, with labels 'A' and 'B' indicating general interior locations for installation.
Installation Detail A (Cockpit/Cabin):
An exploded view illustrates the flashlight assembly (1) and its cradle/charger unit (2). These components are to be attached to a mounting surface (4) using screws (3). The diagram shows the flashlight being inserted into the cradle.
Installation Detail B (Cabin/Baggage):
This detail shows the flashlight (1) and cradle/charger (2) being mounted to a surface (4) with screws (3) and washers (5). A separate view depicts the cradle (2) with the flashlight (1) being inserted, secured by screws (3) and washers (4).
Installation Detail C (Baggage/Other):
Another exploded view shows the flashlight (1) and cradle/charger (2) being mounted to a surface (4) using screws (3).
Parts List for Installation:
| Figure & Index Number | Part Number | Description | Parts Avail. | QTY. Per assy. |
|---|---|---|---|---|
| Option A | ||||
| 1 | AVE-FLA-001 AVE-FLA-P01 AVE-FLA-S01 | Flashlight TheAviator Flashlight TheAviator Pro Flashlight TheAviator Survivor | 1 1 1 | 1 1 1 |
| 2 | MS27039C1-09 | SCREW (PILOT/COPILOT) | 4 | 1 |
| 2A | MS35206-258 | SCREW (BAGGAGE) | 4 | 1 |
| 3 | AN960D10L | WASHER | 4 | 1 |
| 4 | AVE-FCA-001 | Flashlight cradle and charger | 1 | 1 |
| Option B | ||||
| 1 | AVE-FLA-001 AVE-FLA-P01 AVE-FLA-S01 | Flashlight TheAviator Flashlight TheAviator Pro Flashlight TheAviator Survivor | 1 1 1 | 1 1 1 |
| 2 | AVE-FCA-001 | Flashlight cradle and charger | 1 | 1 |
| 3 | MS35649-206 | Nut, self-locking | 4 | 1 |
| 4 | AN960D10L | WASHER | 4 | 1 |
| 5 | MS27039C1-06 | SCREW | 4 | 1 |
| 6 | Original part | Bracket used for original installation | 1 | 1 |
| Option C | ||||
| 1 | AVE-FLA-001 AVE-FLA-P01 AVE-FLA-S01 | Flashlight TheAviator Flashlight TheAviator Pro Flashlight TheAviator Survivor | 1 1 1 | 1 1 1 |
| 2 | MS27039C1-09 | SCREW (PILOT/COPILOT) | 2 | 2 |
| 2A | MS35206-258 | SCREW (BAGGAGE) | 2 | 2 |
| 3 | AN960D10L | WASHER | 2 | 2 |
| 4 | AVE-FCA-001 | Flashlight cradle and charger | 1 | 1 |
Remark and Notes:
Remark: The different options (A, B, C) cater to different interior layouts. Options A and B replace the original MagLite installation found in GII through GVI aircraft. Option C replaces the DME flashlight typically installed in G200 and G280 aircraft.
Notes:
- Remove the existing flashlight and holder according to the Aircraft Maintenance Manual (AMM).
- Disconnect the wiring for the existing flashlight charger.
- Connect the wiring for the new flashlight charger in the same manner as the original installation, using the component installation manual.
- Install the charger using the fastener items listed in the appropriate option. For Option B, if using bolt adhesive Loctite 2400, the charger may be installed horizontally or vertically based on interior and customer preference.
